WO2012076710A1 - Thrust bearing device - Google Patents

Thrust bearing device Download PDF

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Publication number
WO2012076710A1
WO2012076710A1 PCT/EP2011/072382 EP2011072382W WO2012076710A1 WO 2012076710 A1 WO2012076710 A1 WO 2012076710A1 EP 2011072382 W EP2011072382 W EP 2011072382W WO 2012076710 A1 WO2012076710 A1 WO 2012076710A1
Authority
WO
WIPO (PCT)
Prior art keywords
thrust bearing
bearing device
block
deformed
pillow
Prior art date
Application number
PCT/EP2011/072382
Other languages
French (fr)
Inventor
Antonio Gambigliani Zoccoli
Original Assignee
Caprari S.P.A.
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Caprari S.P.A. filed Critical Caprari S.P.A.
Priority to CN201180058817.9A priority Critical patent/CN103249953B/en
Priority to EP11794479.3A priority patent/EP2649323B1/en
Priority to ES11794479T priority patent/ES2739502T3/en
Publication of WO2012076710A1 publication Critical patent/WO2012076710A1/en

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/04Shafts or bearings, or assemblies thereof
    • F04D29/041Axial thrust balancing
    • F04D29/0413Axial thrust balancing hydrostatic; hydrodynamic thrust bearings
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C17/00Sliding-contact bearings for exclusively rotary movement
    • F16C17/02Sliding-contact bearings for exclusively rotary movement for radial load only
    • F16C17/03Sliding-contact bearings for exclusively rotary movement for radial load only with tiltably-supported segments, e.g. Michell bearings
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C17/00Sliding-contact bearings for exclusively rotary movement
    • F16C17/04Sliding-contact bearings for exclusively rotary movement for axial load only
    • F16C17/06Sliding-contact bearings for exclusively rotary movement for axial load only with tiltably-supported segments, e.g. Michell bearings
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C27/00Elastic or yielding bearings or bearing supports, for exclusively rotary movement
    • F16C27/06Elastic or yielding bearings or bearing supports, for exclusively rotary movement by means of parts of rubber or like materials
    • F16C27/063Sliding contact bearings
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C27/00Elastic or yielding bearings or bearing supports, for exclusively rotary movement
    • F16C27/08Elastic or yielding bearings or bearing supports, for exclusively rotary movement primarily for axial load, e.g. for vertically-arranged shafts
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C3/00Shafts; Axles; Cranks; Eccentrics
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C32/00Bearings not otherwise provided for
    • F16C32/06Bearings not otherwise provided for with moving member supported by a fluid cushion formed, at least to a large extent, otherwise than by movement of the shaft, e.g. hydrostatic air-cushion bearings
    • F16C32/0662Details of hydrostatic bearings independent of fluid supply or direction of load
    • F16C32/0666Details of hydrostatic bearings independent of fluid supply or direction of load of bearing pads
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C33/00Parts of bearings; Special methods for making bearings or parts thereof
    • F16C33/02Parts of sliding-contact bearings
    • F16C33/04Brasses; Bushes; Linings
    • F16C33/06Sliding surface mainly made of metal
    • F16C33/10Construction relative to lubrication
    • F16C33/1025Construction relative to lubrication with liquid, e.g. oil, as lubricant
    • F16C33/106Details of distribution or circulation inside the bearings, e.g. details of the bearing surfaces to affect flow or pressure of the liquid
    • F16C33/108Details of distribution or circulation inside the bearings, e.g. details of the bearing surfaces to affect flow or pressure of the liquid with a plurality of elements forming the bearing surfaces, e.g. bearing pads
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2360/00Engines or pumps
    • F16C2360/44Centrifugal pumps

Definitions

  • the thrust bearing devices of the sliding type comprise a couple of substantially flat surfaces on which are distributed the axial loads generated by the functioning of the machine, and between which is provided the formation and maintenance of a fluid film, generally oil or water, necessary for protecting the contacting surfaces in relative motion.
  • a first surface is fixed, so mounted integral to the fixed parts of the machine, while the second surface is mounted integral to the rotating shaft.
  • a further example of known thrust bearing devices is disclosed in patent application US 2004/0066993, relating to an axial bearing of the hydrodynamic type, preferably suitable for the use in hydraulic turbines and comprising a rotor member, a fifth wheel rotating integrally with the shaft of the rotor member and a fixed support segment supported by a containment box.
  • the fifth wheel is constituted by a matrix of plastic material and by reinforcing fibres embedded therein.
  • the technical solutions proposed to date are able to resist efficiently to even considerable axial thrusts but require elevated mechanical precisions, and elevated realization costs, especially for warranting the correct asset of the parts in relative motion.
  • the support segments are usually connected with the containment box through the interposition of spherical coupling means very costly.
  • the containment box usually provides a spherical coupling costly to be realized.
  • the need for an optimization of the efficiency rates is of particular relevance.
  • the task of the present invention is that of solving the aforementioned problems, devising a thrust bearing device of simple and economic conception which allows a reliable functioning.
  • a thrust bearing device comprising a containment box formed by a central sleeve with axis parallel to an axial thrust to be supported, by a ring-shaped support base and by a perimeter wall.
  • a plurality of sliding segments or sliding blocks are arranged inside the containment box, radially distributed around the central sleeve and provided with a support base oriented towards the ring-shaped support base and with an opposite sliding operating surface, conjugated to a corresponding surface portion of a rotor member subjected to the axial thrust and coaxial to the central sleeve.
  • a pillow that can be deformed contained abutting the central sleeve and the perimeter wall, axially interposed between the ring-shaped support base and each of the blocks, to realize a distributed and dynamic asset on each of the blocks.
  • the pillow that can be deformed serves as distributed support for each single block, acting in a dynamic and independent way, like a "water mattress", for the sequence of blocks. [14] Thanks to the pillow that can be deformed the orientation of each block can be registered in a dynamic way, to automatically compensate dimensional shiftings of the components placed in contact and to react to both the static and dynamic thrusts.
  • the pillow that can be deformed is able to contrast such thrusts in a distributed way, the same pillow influences the distribution and the entity of the deformations by compression, so of the subsidings resulting on the operating surface of the blocks.
  • the pillow that can be deformed is suitable to contrast the subsiding of the edges, favouring a local raising of the relative height.
  • Such a raising locally serves as obstacle to the undesired exit of the lubricating fluid interposed between the blocks and the rotor member, to the advantage of the total efficiency rates of the machine in which the device is used.
  • the pillow that can be deformed can be made of rubber and shape a plurality of connection portions for the blocks.
  • connection portions can provide T- shaped profiles guide bodies, distributed and protruding on the same pillow, suitable to engage respective portions of the base of the blocks, to guide the mounting thereof and warrant the axial blocking thereof.
  • figure 1 shows an axial section view of a portion of a centrifugal electric pump in which is used the thrust bearing device according to the invention
  • figure 2 shows a perspective view of the thrust bearing device according to the invention
  • [22] figures 3, 4 and 5 respectively show perspective views of different details of the same thrust bearing device
  • figure 6 shows a perspective view of a further embodiment of the thrust bearing device according to the invention.
  • FIG. 7 [24] figures 7, 8 and 9 respectively show perspective views of different details of the embodiment illustrated in figure 6.
  • a portion of a submerged electric pump is indicated in its entirety with 1 .
  • the electric pump is suitable to pump a liquid, for example water, from an inlet or suction section to an outlet or delivery section through one or more pumping stages, for simplicity not represented in whole.
  • the portion 1 represents a motor unit designed to be coupled to a submerged electric pump.
  • different applications can be provided, for operating or generating machines.
  • the motor unit 1 is preferably realized water-filled or, alternatively filled with another fluid suitable to the cooling and to the lubrication of the parts involved in relative motions, for example oil.
  • the wrapping 2 is suitable to house a motor member 4 of the electric type provided with a motor shaft 5.
  • the shaft 5 is designed to be mechanically connected to the rotating members of one or more pumping stages, handling them in rotational motion about a longitudinal axis A.
  • the motor member 4 is housed inside the wrapping 2 by means of the interposition of a thrust bearing device 10 suitable to equilibrate the axial thrust to which is subjected the motor shaft 5 during the functioning.
  • a rotor member 6 shaping a fifth wheel suitable to transfer the cited axial thrust to the thrust bearing device 10.
  • the fifth wheel 6 together with the thrust bearing device 10 are arranged at one end of the motor shaft 5.
  • the fifth wheel 6 has a ring shape for the insertion coaxial to the motor shaft 5 and presents a sliding operating face 7, substantially flat, suitable to be prearranged, in use, in front of a corresponding operating surface of the thrust bearing device 10, as better described in the following.
  • the operating face 7 of the fifth wheel 6 if preferably realized on a separated component, an insert 8, which can be applied in a corresponding seat of the fifth wheel 6.
  • the fifth wheel 6 is realized in metallic material, for example steel, while the insert 8 is realized in material particularly resistant to wear and tear, for example in impregnated fabric.
  • the microporosities of the fabric favour an effect of drag of the lubricating fluid used inside the motor unit 1 .
  • the thrust bearing device 10 comprises a containment box 1 1 , a plurality of sliding sectors or sliding blocks 12 and a pillow that can be deformed 13 to realize a dynamic support of the blocks 12 (see fig. 2).
  • the containment box 1 1 is on its turn defined by a central sleeve 14, by a substantially flat ring-shaped base 15 and by a containment perimeter wall 16.
  • the perimeter wall 16 externally shapes a threaded portion 17 suitable to the fixing to a corresponding threaded seat 18 realized inside the wrapping 2.
  • the central sleeve 14 has a central opening 19 suitable to allow the insertion of the motor shaft 5 and/or to enable the fixing on the threaded seat 18.
  • the central opening 19 can be made with a hexagonal section, so as to be able to cooperate with a suitable fixing key.
  • the ring-shaped base 15 has preferably a plurality of coupling seats 20, for example having a cylindrical imprint, the function of which is described in the following.
  • Each block 12 has an operating surface 21 suitable in use to receive the axial thrust from the corresponding operating face 7 of the fifth wheel 6 overlapped thereto.
  • the operating surface 21 is preferably and substantially flat in the same way as the fifth wheel 6 or can provide a slightly curved conformation, to produce preferential deformations of the block 12 suitable to make easier the insertion of the lubricating fluid in the meatus defined between the cited operating surfaces.
  • the operating surface 21 is preferably shaped as a circular sector comprised between a minor arc 22 and a major arc 23 and by a couple of radial edges 24.
  • the circular sectors 21 of the blocks 12 are preferably equal, in such a way that in condition of use they can be arranged in sequence shaping a crown on the ring-shaped base 15 of the containment box 1 1 abutting the perimeter wall 16 and the central sleeve 14.
  • Each block has a support base 25 opposite to the operating surface 21 , shaped as a circular sector as well.
  • the support bases 25 of the blocks 12 are preferably arranged in reciprocal contact along a respective radial side 26.
  • the support base 25 further comprises a coupling portion 27 realized for example shaped as a tooth.
  • edges 24 lateral to the operating surface 21 of two different block 12 are preferably not placed in reciprocal contact, but define between them a free space 28 suitable to receive inflowing and to diffuse the lubricating fluid.
  • the cavity 29 of the lateral side produces the overhang conformation of the radial edge 24.
  • Such a conformation allows to perform a controlled and selective sealing at the periphery of the operating surface 21 .
  • the dynamical and distributed support of the block 12 on the pillow 13 reacts to the axial thrust exerted by the shaft 5, determining a spherical concave deformation of the operating surface 21 of the blocks 12.
  • Such a deformation causes a raising of the perimetric edges of the same operating surface 21 , so in the described case of the minor arc 22 and of the major arc 23, with respect to the central region of the operating surface 21 .
  • Such a raising implies a peripheral sealing of the operating surface 21 , obstructing there the passage of the lubricating fluid comprised between the operating surface 21 and the fifth wheel 6.
  • the thickness of the block 12 is enfeebled and made discontinuous by the presence of the cavity 29, the cited localized subsiding effect of the edges 24 overhanging from the lateral side 26 occurs, which contrasts such a raising, allowing there an easy passage of the lubricating fluid. It results thereby a selective sealing of the operating surface 21 , which contrasts the flow of the lubricating fluid in radial direction, retaining it, while it allows and favours the flow of the same fluid in circumferential direction.
  • the protruding radial edges 24 are symmetrical with respect to a median axis of the block 12, favouring in equal measure the inflow and the outflow of fluid in both the rotation senses of the motor shaft 5.
  • the cavity 29 is realized on the entire radial extension of the involved radial side, so the cited axial subsiding involves the entire radial edge 24.
  • the cavity 29 localized in a median or marginal portion of the lateral side of the block 12.
  • the cavity 29 has the shape of a rectangular groove, with curved extension inside the section of the block 12. Such a conformation therefore determines a bigger protruding of the radial edge 24 at a median section of the block 12, and a smaller protruding in proximity of the minor arc 22 and of the major arc 23 respectively, determining preferential subsidings on more or less extended zones in a corresponding way.
  • different solutions can be provided, as an example with the cavity 29 having a rectilinear course along the radial extension of the lateral side, converging or diverging.
  • the cavity 29 is provided preferably on each lateral side of the block 12, in a symmetric way as in figure 5 or asymmetric.
  • Such a provision has the scope of making efficient the "bracket" effect described for any sense of rotation of the motor shaft 5, but also of creating a constant flow of l u bricati ng fl u id th roug h the m eatus , acti ng loca l ly on both the corresponding inlet sections and the outlet ones at the radial edges 24.
  • the blocks 12 are suitable to be arranged in use supported on the pillow 13 that can be deformed.
  • the pillow 13 that can be deformed is thus interposed between the ring-shaped base 15 of the containment box 1 1 and each block 12, abutting the central sleeve 14 and the perimeter wall 16.
  • the pillow 13 that can be deformed has such a conformation as to realize a dynamic support for the blocks 12 arranged thereon. More precisely such a dynamic support allows the blocks 12 axial or angular displacements in order to realize correspondent asset regulations. In particular such regulations serve to compensate the unavoidable dimensional and shape tolerances of the surfaces subjected to relative motion.
  • the pillow 13 that can be deformed is realized according to a structurally continuous solution shaped as a ring, suitable to be contained in the containment box 1 1 and to give each block 12 a support distributed on a corresponding surface.
  • the ring 13 that can be deformed is preferably of elastic material of the rubber type, to enable the dynamic and interdependent re-asset of the blocks 12.
  • the ring 13 that can be deformed can be of different materials that can be deformed, for example of the plastic type.
  • the ring 13 that can be deformed comprises preferably a plurality of coupling elements 30 suitable to the connection with the cited coupling seats 20 realized in the ring-shaped base 15 for the angular and radial fixing of the same ring.
  • connection portions 31 designed to be associated with the respective coupling portions 27 of the blocks 12. More precisely, in the illustrated case the connection portions 31 are shaped by radial grooves having a shape suitable to receive the teeth 27 of each block 12 for the correct radial and axial positioning.
  • the shape of such radial grooves 31 and so of the relative coupling teeth 27 can be anyone provided that it is suitable to the cited scope of reciprocal positioning.
  • Figure 6 illustrates a second embodiment of the thrust bearing device 10 according to the invention, wherein the technical characteristics functionally corresponding to the previously described ones are indicated with the same number.
  • connection portions 310 which protrude axially from the support surface for the blocks 12.
  • the connection portions 310 are interposed to the blocks 12, preferably radially distributed.
  • the connection portions 310 have a substantially dovetail profile, as defined by a radial guide rib 320 carrying transverse borders 330 at the top, in such a way as to define between the pillow 13 and the borders 330 a guide space 340.
  • the space 340 serves to house and axially block respective end portions of the support surface 25 of a couple of adjacent blocks 12 (see figures 6 and 8).
  • the connection portions 310 therefore serve as a guide to the blocks 12 during the mounting on the pillow 13 and as a blocking to the axial displacement of the same blocks 12.
  • the pillow 13 that can be deformed can be realized by a structurally discontinuous support.
  • the cited dynamic support function is realized by a pillow of macroscopic particles, for example microspheres or granules, free to slide on each other in a dynamic way as a response to an axial thrust. Therefore, as in the embodiment previously described, the conformation of the pillow of particles can be seen as capable of being deformed in a dynamic way.
  • each particle has dimensions sufficiently reduced to ensure for each block 12 a support distributed on the major number of points and in the meanwhile dimensions sufficiently elevated to avoid the exit thereof from the chamber defined between the support plane of the blocks 12, the central sleeve 14, the ring-shaped base 15 and the perimeter wall 16.
  • the thrust bearing device 10 is prearranged inside the wrapping 2 wherein is mounted the motor member 4, by fixing the containment box 1 1 in the relative fixing seat of the wrapping 2.
  • Each sliding block 12 is automatically registered, each block arranging by itself in contact with a corresponding surface portion of the fifth wheel 6. Thanks to the aptitude to be deformed of the pillow 13 inside the containment box 1 1 , in fact each block 12 undergoes a registration in axial sense, aligning its own axial height with the one of the remaining blocks 12, and in angular sense, tilting accordingly.
  • the weight of the motor unit 1 and of the machine connected thereto results sustained by the thrust bearing device 10 through transfer of the corresponding axial thrust through the fifth wheel 6, the blocks 12 and the pillow 13 that can be deformed.
  • the fifth wheel 6 slides on the sequence of blocks 12 of the thrust bearing device 10. Thanks to the dynamic support made possible by the pillow 13 that can be deformed the blocks 12 can vary their own asset in a dynamic way as a response to the axial thrust transmitted by the fifth wheel 6. In particular the blocks 12 can be subjected to dynamic compensation displacements, of tilting or of translation to adapt instantaneously their own asset to the operating face 7 of the fifth wheel 6.
  • the thrust bearing device according to the invention therefore attains the scope of enabling a reliable functioning at elevated yields. Such a scope is reached in particular by providing the pillow 13 that can be deformed, for the reasons and the effects previously highlighted.
  • the thrust bearing device is able to optimize the efficiency rates, reducing the losses due to friction to the minimum, thanks to the cited protruding edges 24.
  • these edges 24 favour the continuous recirculation of a suitable film of lubricating fluid in the meatus between the blocks and the rotor member.
  • a characteristic of the thrust bearing device according to the invention is given by the fact that it is based on a constructively simple technical solution, which therefore requires reduced realization costs.
  • the proposed solution requires lower mechanical precisions and so lower costs with respect to the known solutions, warranting in the meantime more elevated efficiency rates.

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Chemical & Material Sciences (AREA)
  • Oil, Petroleum & Natural Gas (AREA)
  • Ocean & Marine Engineering (AREA)
  • Sliding-Contact Bearings (AREA)
  • Support Of The Bearing (AREA)

Abstract

The thrust bearing device suitable to support an axial thrust through a shaft (5) comprises a containment box (11) formed by a central sleeve (14) according to an axis (A) parallel in use to the axial thrust to be supported, a ring-shaped support base (15) and a perimeter wall (16), a plurality of sliding sectors or sliding blocks (12) arranged inside the containment box (11), radially distributed around the central sleeve (14) and provided with a support base (25) oriented in use towards the ring-shaped support base (15) and with a sliding operating surface (21) suitable to be arranged faced to a corresponding surface of a rotor member integral to the shaft (5).A pillow that can be deformed (13) is contained abutting the central sleeve (14) and the perimeter wall (16), being axially interposed between the ring-shaped support base (15) and each of the sliding blocks (12).

Description

Description
THRUST BEARING DEVICE
Technical Field
[01 ] The present invention regards a thrust bearing device, in particular for centrifugal pumps.
Background Art
[02] The use of so-called "Michell" type of thrust bearing devices has been known, for supporting even elevated axial thrusts generated in the functioning of generator machines, for example hydraulic turbines or operating machines, such as centrifugal pumps.
[03] Such known thrust bearing devices are illustrated by patent GB 190500875 on behalf A. G. M. Michell who was the first to develop in 1905 a technical solution based on the concept of dynamic support operated through thrust bearing devices of the sliding type.
[04] In general, the thrust bearing devices of the sliding type comprise a couple of substantially flat surfaces on which are distributed the axial loads generated by the functioning of the machine, and between which is provided the formation and maintenance of a fluid film, generally oil or water, necessary for protecting the contacting surfaces in relative motion. A first surface is fixed, so mounted integral to the fixed parts of the machine, while the second surface is mounted integral to the rotating shaft.
[05] The idea developed by Michell and illustrated in the cited patent consists in subdividing the first sliding surface in a plurality of adjacent sectors, thus making it discontinuous. According to the proposed solution, each sector is mounted tilting on a spherical support, in order to warrant an optimal hydrodynamic maintenance in any functioning condition. More precisely, the provision of a plurality of independent sectors and of spherical supports for each of them warrants at the same time the correct axial positioning and an optimal dynamic asset for interposing a film of fluid in sufficient measure, between the first fixed sliding surface and the second surface mobile in rotation.
A further example of known thrust bearing devices is disclosed in patent application US 2004/0066993, relating to an axial bearing of the hydrodynamic type, preferably suitable for the use in hydraulic turbines and comprising a rotor member, a fifth wheel rotating integrally with the shaft of the rotor member and a fixed support segment supported by a containment box. According to such a technical solution the fifth wheel is constituted by a matrix of plastic material and by reinforcing fibres embedded therein. The technical solutions proposed to date are able to resist efficiently to even considerable axial thrusts but require elevated mechanical precisions, and elevated realization costs, especially for warranting the correct asset of the parts in relative motion. To such an end it's enough to note that the support segments are usually connected with the containment box through the interposition of spherical coupling means very costly. Equally the containment box usually provides a spherical coupling costly to be realized. Furthermore in the specified sector of use, in particular in the one of the operating machines of the type of the centrifugal pumps, the need for an optimization of the efficiency rates is of particular relevance.
Disclosure
The task of the present invention is that of solving the aforementioned problems, devising a thrust bearing device of simple and economic conception which allows a reliable functioning.
[10] Another scope of the invention is that of providing a thrust bearing device which allows to obtain elevated efficiency rates.
[1 1 ] Within such task, it is a further scope of the present invention that of providing a thrust bearing device suitable to be used in a centrifugal pump and to warrant an optimal functioning.
[12] The cited scopes are attained, according to the present invention, by the thrust bearing device according to claim 1 , as well as by the centrifugal pump according to claim 10.
[13] In particular the scopes are attained by means of a thrust bearing device comprising a containment box formed by a central sleeve with axis parallel to an axial thrust to be supported, by a ring-shaped support base and by a perimeter wall. A plurality of sliding segments or sliding blocks are arranged inside the containment box, radially distributed around the central sleeve and provided with a support base oriented towards the ring-shaped support base and with an opposite sliding operating surface, conjugated to a corresponding surface portion of a rotor member subjected to the axial thrust and coaxial to the central sleeve. Also provided is a pillow that can be deformed contained abutting the central sleeve and the perimeter wall, axially interposed between the ring-shaped support base and each of the blocks, to realize a distributed and dynamic asset on each of the blocks. In practice the pillow that can be deformed serves as distributed support for each single block, acting in a dynamic and independent way, like a "water mattress", for the sequence of blocks. [14] Thanks to the pillow that can be deformed the orientation of each block can be registered in a dynamic way, to automatically compensate dimensional shiftings of the components placed in contact and to react to both the static and dynamic thrusts. Given that the pillow that can be deformed is able to contrast such thrusts in a distributed way, the same pillow influences the distribution and the entity of the deformations by compression, so of the subsidings resulting on the operating surface of the blocks. In other words the pillow that can be deformed is suitable to contrast the subsiding of the edges, favouring a local raising of the relative height. Such a raising locally serves as obstacle to the undesired exit of the lubricating fluid interposed between the blocks and the rotor member, to the advantage of the total efficiency rates of the machine in which the device is used.
[15] According to the invention the formation and maintenance of a suitable film of fluid results made easier between the blocks and the rotating surface of the rotor member placed in contact. Such a scope is attained thanks to the provision of a lateral side of the block, carrying a cavity or notch such as to shape a localized enfeeblement of the transverse section of the block, with a so-called "bracket" effect. More precisely the presence of the cavity or notch in the lateral side of the block determines a lateral edge protruding overhang from the operating surface of the block, such as to warrant a preferential subsiding under effect of the application of the axial thrust.
[16] In practice when the protruding edge is subjected to the axial thrust transmitted by the rotor member, it behaves as a bracket and so gets deformed bending itself. Such a flexure substantially represents a subsiding due to the enfeeblement localized in the thickness of the lateral side of the block and has the effect of locally broadening the section of the meatus defined between blocks and rotor member. Thus the inflow and/or outflow of the lubricating fluid on the block turns out favoured, at the advantage of the hydrodynamic maintenance of the thrust bearing device. Such subsidings are preferably of the elastic type, so suitable to generate dynamic subsidings of the edges during the functioning.
The combination of such effects, the sealing of the internal and external edges of the blocks and the selective opening of the lateral bracket edges, enables to obtain efficiency rates at least doubled with respect to the ones that can be obtained through the known devices.
Furthermore, according to a particular aspect of the invention, the pillow that can be deformed can be made of rubber and shape a plurality of connection portions for the blocks. Such connection portions can provide T- shaped profiles guide bodies, distributed and protruding on the same pillow, suitable to engage respective portions of the base of the blocks, to guide the mounting thereof and warrant the axial blocking thereof.
Description of Drawings
Details of the invention shall be more apparent from the detailed description of a preferred embodiment of the thrust bearing device according to the invention, illustrated for indicative purposes in the attached drawings, wherein:
figure 1 shows an axial section view of a portion of a centrifugal electric pump in which is used the thrust bearing device according to the invention; figure 2 shows a perspective view of the thrust bearing device according to the invention; [22] figures 3, 4 and 5 respectively show perspective views of different details of the same thrust bearing device;
[23] figure 6 shows a perspective view of a further embodiment of the thrust bearing device according to the invention;
[24] figures 7, 8 and 9 respectively show perspective views of different details of the embodiment illustrated in figure 6.
Best Mode
[25] With particular reference to such figures, a portion of a submerged electric pump is indicated in its entirety with 1 . The electric pump is suitable to pump a liquid, for example water, from an inlet or suction section to an outlet or delivery section through one or more pumping stages, for simplicity not represented in whole. In the illustrated case the portion 1 represents a motor unit designed to be coupled to a submerged electric pump. Alternatively different applications can be provided, for operating or generating machines.
[26] The motor unit 1 is preferably realized water-filled or, alternatively filled with another fluid suitable to the cooling and to the lubrication of the parts involved in relative motions, for example oil.
[27] The motor unit 1 comprises a cylindrical wrapping 2 closed at one end by a cover 3 and provided at the opposite end with a connection portion, for coupling with the user machine, for example an electric pump or another machine.
[28] The wrapping 2 is suitable to house a motor member 4 of the electric type provided with a motor shaft 5. As an example the shaft 5 is designed to be mechanically connected to the rotating members of one or more pumping stages, handling them in rotational motion about a longitudinal axis A.
The motor member 4 is housed inside the wrapping 2 by means of the interposition of a thrust bearing device 10 suitable to equilibrate the axial thrust to which is subjected the motor shaft 5 during the functioning.
More precisely on the motor shaft 5 of the motor member 4 is present a rotor member 6 shaping a fifth wheel suitable to transfer the cited axial thrust to the thrust bearing device 10. In the illustrated case the fifth wheel 6 together with the thrust bearing device 10 are arranged at one end of the motor shaft 5. In alternative it is possible to provide different dispositions, for example mounting the fifth wheel 6 and the thrust bearing device 10 at a median portion of the motor shaft 5.
The fifth wheel 6 has a ring shape for the insertion coaxial to the motor shaft 5 and presents a sliding operating face 7, substantially flat, suitable to be prearranged, in use, in front of a corresponding operating surface of the thrust bearing device 10, as better described in the following.
The operating face 7 of the fifth wheel 6 if preferably realized on a separated component, an insert 8, which can be applied in a corresponding seat of the fifth wheel 6.
Preferably the fifth wheel 6 is realized in metallic material, for example steel, while the insert 8 is realized in material particularly resistant to wear and tear, for example in impregnated fabric. In this case the microporosities of the fabric favour an effect of drag of the lubricating fluid used inside the motor unit 1 .
The thrust bearing device 10 comprises a containment box 1 1 , a plurality of sliding sectors or sliding blocks 12 and a pillow that can be deformed 13 to realize a dynamic support of the blocks 12 (see fig. 2).
[35] The containment box 1 1 is on its turn defined by a central sleeve 14, by a substantially flat ring-shaped base 15 and by a containment perimeter wall 16.
[36] The perimeter wall 16 externally shapes a threaded portion 17 suitable to the fixing to a corresponding threaded seat 18 realized inside the wrapping 2. The central sleeve 14 has a central opening 19 suitable to allow the insertion of the motor shaft 5 and/or to enable the fixing on the threaded seat 18. In this latter case for example the central opening 19 can be made with a hexagonal section, so as to be able to cooperate with a suitable fixing key.
[37] The ring-shaped base 15 has preferably a plurality of coupling seats 20, for example having a cylindrical imprint, the function of which is described in the following.
[38] Each block 12 has an operating surface 21 suitable in use to receive the axial thrust from the corresponding operating face 7 of the fifth wheel 6 overlapped thereto. The operating surface 21 is preferably and substantially flat in the same way as the fifth wheel 6 or can provide a slightly curved conformation, to produce preferential deformations of the block 12 suitable to make easier the insertion of the lubricating fluid in the meatus defined between the cited operating surfaces. The operating surface 21 is preferably shaped as a circular sector comprised between a minor arc 22 and a major arc 23 and by a couple of radial edges 24. The circular sectors 21 of the blocks 12 are preferably equal, in such a way that in condition of use they can be arranged in sequence shaping a crown on the ring-shaped base 15 of the containment box 1 1 abutting the perimeter wall 16 and the central sleeve 14.
[39] Each block has a support base 25 opposite to the operating surface 21 , shaped as a circular sector as well. The support bases 25 of the blocks 12 are preferably arranged in reciprocal contact along a respective radial side 26. The support base 25 further comprises a coupling portion 27 realized for example shaped as a tooth.
[40] It is to be noted that unlike the radial sides 26 at the sides of the support base 25, the edges 24 lateral to the operating surface 21 of two different block 12 are preferably not placed in reciprocal contact, but define between them a free space 28 suitable to receive inflowing and to diffuse the lubricating fluid.
[41 ] It is also important to underline that at least at a lateral wall of the block 12, preferably on a lateral side, is provided a cavity 29 suitable to enfeeble locally the transverse section of the block 12. Therefore the radial edge 24 results protruding overhang from the same lateral side in corresponding measure. The cavity 29 or an equivalent conformation which makes protruding the radial edge 24 produces in substance a "bracket" effect. In other words, under effect of the described protruding conformation, the radial edge 24 is subject to preferential localized subsidings following the application of an axial thrust on the operating surface 21 . Such preferential subsidings produce a localized increase of the transverse section of the meatus defined between the operating surface 21 and the fifth wheel 6, facilitating at the radial edges 24 the circulation of the lubricating fluid. In such a way an optimal thickness of lubricating fluid suitable to make minimal the losses by sliding friction is always warranted.
It is to be underlined that the cavity 29 of the lateral side produces the overhang conformation of the radial edge 24. Such a conformation allows to perform a controlled and selective sealing at the periphery of the operating surface 21 . In other words, the dynamical and distributed support of the block 12 on the pillow 13 reacts to the axial thrust exerted by the shaft 5, determining a spherical concave deformation of the operating surface 21 of the blocks 12. Such a deformation causes a raising of the perimetric edges of the same operating surface 21 , so in the described case of the minor arc 22 and of the major arc 23, with respect to the central region of the operating surface 21 . Such a raising implies a peripheral sealing of the operating surface 21 , obstructing there the passage of the lubricating fluid comprised between the operating surface 21 and the fifth wheel 6. In the other hand where the thickness of the block 12 is enfeebled and made discontinuous by the presence of the cavity 29, the cited localized subsiding effect of the edges 24 overhanging from the lateral side 26 occurs, which contrasts such a raising, allowing there an easy passage of the lubricating fluid. It results thereby a selective sealing of the operating surface 21 , which contrasts the flow of the lubricating fluid in radial direction, retaining it, while it allows and favours the flow of the same fluid in circumferential direction. In the illustrated embodiment the protruding radial edges 24 are symmetrical with respect to a median axis of the block 12, favouring in equal measure the inflow and the outflow of fluid in both the rotation senses of the motor shaft 5. In alternative it is possible to provide one only protruding radial edge 24 for each block 12 or protruding edges on both the lateral sides, but shaped in asymmetric manner, for example not completely radial, influencing in a differentiated way the inflow and the outflow of the fluid in the meatus.
[44] In the case illustrated in figure 5 the cavity 29 is realized on the entire radial extension of the involved radial side, so the cited axial subsiding involves the entire radial edge 24. In alternative it is possible to provide different realizations, for example with the cavity 29 localized in a median or marginal portion of the lateral side of the block 12.
[45] In the illustrated case the cavity 29 has the shape of a rectangular groove, with curved extension inside the section of the block 12. Such a conformation therefore determines a bigger protruding of the radial edge 24 at a median section of the block 12, and a smaller protruding in proximity of the minor arc 22 and of the major arc 23 respectively, determining preferential subsidings on more or less extended zones in a corresponding way. In alternative, different solutions can be provided, as an example with the cavity 29 having a rectilinear course along the radial extension of the lateral side, converging or diverging.
[46] Furthermore the cavity 29 is provided preferably on each lateral side of the block 12, in a symmetric way as in figure 5 or asymmetric. Such a provision has the scope of making efficient the "bracket" effect described for any sense of rotation of the motor shaft 5, but also of creating a constant flow of l u bricati ng fl u id th roug h the m eatus , acti ng loca l ly on both the corresponding inlet sections and the outlet ones at the radial edges 24.
[47] The blocks 12 are suitable to be arranged in use supported on the pillow 13 that can be deformed. The pillow 13 that can be deformed is thus interposed between the ring-shaped base 15 of the containment box 1 1 and each block 12, abutting the central sleeve 14 and the perimeter wall 16. The pillow 13 that can be deformed has such a conformation as to realize a dynamic support for the blocks 12 arranged thereon. More precisely such a dynamic support allows the blocks 12 axial or angular displacements in order to realize correspondent asset regulations. In particular such regulations serve to compensate the unavoidable dimensional and shape tolerances of the surfaces subjected to relative motion.
[48] In the illustrated case the pillow 13 that can be deformed is realized according to a structurally continuous solution shaped as a ring, suitable to be contained in the containment box 1 1 and to give each block 12 a support distributed on a corresponding surface. In this case, the ring 13 that can be deformed is preferably of elastic material of the rubber type, to enable the dynamic and interdependent re-asset of the blocks 12. In alternative the ring 13 that can be deformed can be of different materials that can be deformed, for example of the plastic type.
[49] The ring 13 that can be deformed comprises preferably a plurality of coupling elements 30 suitable to the connection with the cited coupling seats 20 realized in the ring-shaped base 15 for the angular and radial fixing of the same ring.
[50] At the side of the ring 13 that can be deformed suitable to support the base 25 of the blocks 12 are preferably provided connection portions 31 designed to be associated with the respective coupling portions 27 of the blocks 12. More precisely, in the illustrated case the connection portions 31 are shaped by radial grooves having a shape suitable to receive the teeth 27 of each block 12 for the correct radial and axial positioning. The shape of such radial grooves 31 and so of the relative coupling teeth 27 can be anyone provided that it is suitable to the cited scope of reciprocal positioning.
[51 ] Figure 6 illustrates a second embodiment of the thrust bearing device 10 according to the invention, wherein the technical characteristics functionally corresponding to the previously described ones are indicated with the same number.
[52] At the difference of what is already described, in the case illustrated in the figures from 6 to 9 the pillow that can be deformed 13 comprises connection portions 310 which protrude axially from the support surface for the blocks 12. The connection portions 310 are interposed to the blocks 12, preferably radially distributed. In particular the connection portions 310 have a substantially dovetail profile, as defined by a radial guide rib 320 carrying transverse borders 330 at the top, in such a way as to define between the pillow 13 and the borders 330 a guide space 340. The space 340 serves to house and axially block respective end portions of the support surface 25 of a couple of adjacent blocks 12 (see figures 6 and 8). The connection portions 310 therefore serve as a guide to the blocks 12 during the mounting on the pillow 13 and as a blocking to the axial displacement of the same blocks 12.
[53] According to a different embodiment, not represented, the pillow 13 that can be deformed can be realized by a structurally discontinuous support. In this case the cited dynamic support function is realized by a pillow of macroscopic particles, for example microspheres or granules, free to slide on each other in a dynamic way as a response to an axial thrust. Therefore, as in the embodiment previously described, the conformation of the pillow of particles can be seen as capable of being deformed in a dynamic way. Moreover each particle has dimensions sufficiently reduced to ensure for each block 12 a support distributed on the major number of points and in the meanwhile dimensions sufficiently elevated to avoid the exit thereof from the chamber defined between the support plane of the blocks 12, the central sleeve 14, the ring-shaped base 15 and the perimeter wall 16.
The functioning of the thrust bearing device according to the invention turns out to be easy to understand from the preceding description.
In mounting phase the thrust bearing device 10 is prearranged inside the wrapping 2 wherein is mounted the motor member 4, by fixing the containment box 1 1 in the relative fixing seat of the wrapping 2. Each sliding block 12 is automatically registered, each block arranging by itself in contact with a corresponding surface portion of the fifth wheel 6. Thanks to the aptitude to be deformed of the pillow 13 inside the containment box 1 1 , in fact each block 12 undergoes a registration in axial sense, aligning its own axial height with the one of the remaining blocks 12, and in angular sense, tilting accordingly. In particular the weight of the motor unit 1 and of the machine connected thereto results sustained by the thrust bearing device 10 through transfer of the corresponding axial thrust through the fifth wheel 6, the blocks 12 and the pillow 13 that can be deformed.
When the motor member is actuated, the motor shaft 5 is driven in rotation together with the rotating members of the pump connected thereto. The components set in rotation result stressed by various thrusts, between which an axial thrust in direction of the axis A.
[58] Further to the rotation of the motor shaft 5 the fifth wheel 6 slides on the sequence of blocks 12 of the thrust bearing device 10. Thanks to the dynamic support made possible by the pillow 13 that can be deformed the blocks 12 can vary their own asset in a dynamic way as a response to the axial thrust transmitted by the fifth wheel 6. In particular the blocks 12 can be subjected to dynamic compensation displacements, of tilting or of translation to adapt instantaneously their own asset to the operating face 7 of the fifth wheel 6.
[59] The thrust bearing device according to the invention therefore attains the scope of enabling a reliable functioning at elevated yields. Such a scope is reached in particular by providing the pillow 13 that can be deformed, for the reasons and the effects previously highlighted.
[60] Furthermore the thrust bearing device is able to optimize the efficiency rates, reducing the losses due to friction to the minimum, thanks to the cited protruding edges 24. In fact these edges 24 favour the continuous recirculation of a suitable film of lubricating fluid in the meatus between the blocks and the rotor member.
[61 ] A characteristic of the thrust bearing device according to the invention is given by the fact that it is based on a constructively simple technical solution, which therefore requires reduced realization costs. In particular the proposed solution requires lower mechanical precisions and so lower costs with respect to the known solutions, warranting in the meantime more elevated efficiency rates.
[62] It is further to be observed that the proposed solution requires a minor number of mechanical pieces with respect to the known solutions of thrust bearing devices, further contributing to the reduction of the realization costs.
[63] In practice, the embodiment of the invention, the materials used, as well as the shape and dimensions, may vary depending on the requirements.
[64] Should the technical characteristics mentioned in each claim be followed by reference signs, such reference signs were included strictly with the aim of enhancing the understanding of the claims and hence they shall not be deemed restrictive in any manner whatsoever on the scope of each element identified for exemplifying purposes by such reference signs.

Claims

Claims Thrust bearing device, in particular for centrifugal electric pumps, suitable to support an axial thrust through a shaft (5), comprising
a containment box (1 1 ) formed by a central sleeve (14) with axis (A) parallel in use to said axial thrust, a ring-shaped support base (15) and a perimeter wall (16);
a plurality of sliding sectors or sliding blocks (12) arranged inside said containment box (1 1 ), radially distributed around said central sleeve (14) and provided with a support base (25) oriented in use towards said ring- shaped support base (15) and having a sliding operating surface (21 ) suitable to be arranged faced to a corresponding surface of a rotor member integral to said shaft (5),
a pillow that can be deformed (13) contained abutting said central shaft (14) and said perimeter wall (16) and axially interposed between said ring- shaped support base (15) and each of said sliding blocks (12), in order to function as a distributed and dynamical support for said sliding blocks;
characterized in that
said block (12) comprises a cavity (29) made along a radial side of the same block (12), said cavity (29) determining in said sliding operating surface (21 ) the formation of a protruding edge (24) overhang from said radial side of the block (12), to locally enfeeble the transverse section of the block (12) and allowing a preferential subsiding of said protruding edge (24) under effect of said axial thrust, such as to favour the circulation of a film of lubricating fluid in the meatus between said block (12) and said rotor member (6).
2. Thrust bearing device according to claim 1 , characterized in that said cavity (29) is shaped as a rectangular groove.
3. Thrust bearing device according to claim 2, characterized in that said rectangular shaped cavity (29) extends with a bent course inside the section of said sliding block (12).
4. Thrust bearing device according to claim 1 or 2, characterized in that it comprises a couple of protruding edges (24), each protruding edge (24) being overhang from a respective said radial side of said block (12), to favour both the inflow and the outflow of said film of lubricating fluid in circumferential direction.
5. Thrust bearing device according to claim 4, characterized in that said couple of protruding edges (24) has an axial symmetric conformation.
6. Thrust bearing device according to claim 1 , characterized in that said pillow that can be deformed (13) is realized by means of a structurally continuous solution, comprising a ring made of a material that can be deformed, such as to contrast said axial thrust, producing the selective sealing at the edges of said operating surface (21 ).
7. Thrust bearing device according to one or more of the previous claims, characterized in that said ring (13) that can be deformed is made of rubber.
8. Thrust bearing device according to claim 7, characterized in that said pillow that can be deformed (13) has portions (310) for connecting to said blocks (12), said connection portions (310) having a substantially dovetail profile, in a way as to guide radially and block axially said blocks (12).
9. Thrust bearing device according to one or more of the previous claims, characterized in that pillow that can be deformed (1 3) is realized by means of a structurally discontinuous support, shaping a pillow of macroscopic particles, for example microspheres or granules, free to skid on one another in a dynamical manner in response to said axial thrust. Centrifugal pump comprising a thrust bearing device according to one or more of the previous claims.
PCT/EP2011/072382 2010-12-10 2011-12-09 Thrust bearing device WO2012076710A1 (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
CN201180058817.9A CN103249953B (en) 2010-12-10 2011-12-09 Thrust bearing device
EP11794479.3A EP2649323B1 (en) 2010-12-10 2011-12-09 Thrust bearing device
ES11794479T ES2739502T3 (en) 2010-12-10 2011-12-09 Thrust bearing device

Applications Claiming Priority (2)

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ITBO2010A000730A IT1402832B1 (en) 2010-12-10 2010-12-10 DRAWING DEVICE
ITBO2010A000730 2010-12-10

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WO2012076710A1 true WO2012076710A1 (en) 2012-06-14

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CN (1) CN103249953B (en)
ES (1) ES2739502T3 (en)
IT (1) IT1402832B1 (en)
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WO (1) WO2012076710A1 (en)

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CN112334663A (en) * 2018-07-02 2021-02-05 Ksb股份有限公司 Assembly for absorbing axial thrust of centrifugal pump
CN114382776A (en) * 2021-12-17 2022-04-22 哈尔滨电气动力装备有限公司 Nuclear main pump thrust tile static water layer heat insulation structure

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JP6804578B2 (en) * 2019-02-08 2020-12-23 大同メタル工業株式会社 Half-thrust bearing for crankshaft of internal combustion engine

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DE868087C (en) * 1951-11-18 1953-02-23 Egon Dr-Ing Martyrer Thrust bearing
DD203601A1 (en) * 1982-02-05 1983-10-26 Juergen Bradschetl HYDRAULIC LOAD COMPENSATION FOR PRESSURE STONES FROM AXIAL SLIDING BEARINGS
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Publication number Priority date Publication date Assignee Title
CN112334663A (en) * 2018-07-02 2021-02-05 Ksb股份有限公司 Assembly for absorbing axial thrust of centrifugal pump
CN112334663B (en) * 2018-07-02 2023-09-29 Ksb股份有限公司 Assembly for absorbing axial thrust of centrifugal pump
CN114382776A (en) * 2021-12-17 2022-04-22 哈尔滨电气动力装备有限公司 Nuclear main pump thrust tile static water layer heat insulation structure
CN114382776B (en) * 2021-12-17 2024-05-17 哈尔滨电气动力装备有限公司 Nuclear main pump thrust tile static water layer heat insulation structure

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Publication number Publication date
EP2649323B1 (en) 2019-05-01
CN103249953B (en) 2015-11-25
EP2649323A1 (en) 2013-10-16
IT1402832B1 (en) 2013-09-27
TR201911271T4 (en) 2019-08-21
ITBO20100730A1 (en) 2012-06-11
CN103249953A (en) 2013-08-14
ES2739502T3 (en) 2020-01-31

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